DocumentCode
3406480
Title
Effects of the shape of compressor characteristics on actuator requirements for rotating stall control
Author
Wang, Yong ; Murray, Richard M.
Author_Institution
Div. of Eng. & Appl. Sci., California Inst. of Technol., Pasadena, CA, USA
Volume
4
fYear
1998
fDate
21-26 Jun 1998
Firstpage
1996
Abstract
We present a systematic analysis on the effects of noise, the shape of compressor characteristics, and bleed valve actuator limits on the performance of controllers in rotating stall control. We use center manifold reduction to the three state Moore Greitzer model with piecewise analytic compressor characteristics. For the reduced system, the optimal control which achieves the largest operability enhancement is the “bang-on” control law that drives the valve to open against its rate limit. For the optimal controller, we also derive approximate formulas for the operability enhancement as a function of the noise level, the actuator limits, and the shape of compressor characteristics. The predictions by the formulas are compared with numerical simulations using a model for a low speed axial compressor
Keywords
actuators; aerospace engines; compressors; control system synthesis; optimal control; valves; actuator requirements; bang-on control law; bleed valve actuator limits; compressor characteristics; low speed axial compressor; noise level; operability enhancement; optimal control; rotating stall control; systematic analysis; three state Moore Greitzer model; Actuators; Control systems; Noise level; Noise shaping; Numerical simulation; Optimal control; Performance analysis; Predictive models; Shape control; Valves;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1998. Proceedings of the 1998
Conference_Location
Philadelphia, PA
ISSN
0743-1619
Print_ISBN
0-7803-4530-4
Type
conf
DOI
10.1109/ACC.1998.702975
Filename
702975
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